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Related PDFs (11)

Elementary Flows

Formulas : 16 Size : 335 kb

Elliptical Lift Distribution

Formulas : 20 Size : 349 kb

Flow and Lift Distribution

Formulas : 24 Size : 394 kb

Flow over Airfoils and Wings

Formulas : 26 Size : 421 kb

Fundamentals of Inviscid and Incompressible Flow

Formulas : 16 Size : 342 kb

Lift Distribution

Formulas : 30 Size : 426 kb

Lifting Flow over Cylinder

Formulas : 10 Size : 300 kb

Nonlifting Flow over Cylinder

Formulas : 10 Size : 296 kb

Normal Shock Wave

Formulas : 35 Size : 468 kb

Oblique Shock and Expansion Waves

Formulas : 20 Size : 390 kb

Three-Dimensional Incompressible Flow

Formulas : 29 Size : 419 kb

Critical Density

Critical Pressure

Critical Temperature

Flow Velocity Downstream of Sound Wave

Flow Velocity Upstream of Sound Wave

Isentropic Change across Sound Wave

Isentropic Compressibility for given Density and Speed of Sound

Mach Angle

Mach Number

Mayer's Formula

Ratio of Stagnation and Static Density

Ratio of Stagnation and Static Pressure

Ratio of Stagnation and Static Temperature

Speed of Sound

Speed of Sound Downstream of Sound Wave

Speed of Sound given Isentropic Change

Speed of Sound Upstream of Sound Wave

Stagnation Temperature

a Speed of Sound (Meter per Second)
a₁ Sound Speed Upstream (Meter per Second)
a₂ Sound Speed Downstream (Meter per Second)
C_p Specific Heat Capacity at Constant Pressure (Joule per Kilogram per K)
C_v Specific Heat Capacity at Constant Volume (Joule per Kilogram per K)
dpdρ Isentropic Change (Square Meter per Square Second)
M Mach Number
P₀ Stagnation Pressure (Atmosphere Technical)
p_cr Critical Pressure (Atmosphere Technical)
P_r Stagnation to Static Pressure
R Specific Gas Constant (Joule per Kilogram per K)
T₀ Stagnation Temperature (Kelvin)
T_cr Critical Temperature (Kelvin)
T_r Stagnation to Static Temperature
T_s Static Temperature (Kelvin)
u₁ Flow Velocity Upstream of Sound (Meter per Second)
u₂ Flow Velocity Downstream of Sound (Meter per Second)
V_b Speed of Object (Meter per Second)
γ Specific Heat Ratio
μ Mach Angle (Degree)
ρ Density (Kilogram per Cubic Meter)
ρ_cr Critical Density (Kilogram per Cubic Meter)
ρ_o Stagnation Density (Kilogram per Cubic Meter)
ρ_r Stagnation to Static Density
𝜏_s Isentropic Compressibility (Square Centimeter per Newton)

Constant: [R-Dry-Air], 287.058
Specific Gas Constant for Dry Air
Function: asin, asin(Number)
The inverse sine function, is a trigonometric function that takes a ratio of two sides of a right triangle and outputs the angle opposite the side with the given ratio.
Function: sin, sin(Angle)
Sine is a trigonometric function that describes the ratio of the length of the opposite side of a right triangle to the length of the hypotenuse.
Function: sqrt, sqrt(Number)
A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number.
Measurement: Temperature in Kelvin (K)
Temperature Unit Conversion
Measurement: Pressure in Atmosphere Technical (at)
Pressure Unit Conversion
Measurement: Speed in Meter per Second (m/s)
Speed Unit Conversion
Measurement: Angle in Degree (°)
Angle Unit Conversion
Measurement: Specific Heat Capacity in Joule per Kilogram per K (J/(kg*K))
Specific Heat Capacity Unit Conversion
Measurement: Density in Kilogram per Cubic Meter (kg/m³)
Density Unit Conversion
Measurement: Specific Energy in Square Meter per Square Second (m²/s²)
Specific Energy Unit Conversion
Measurement: Compressibility in Square Centimeter per Newton (cm²/N)
Compressibility Unit Conversion